Buckling behavior of variable-stiffness composite laminates manufactured by the tow-drop method

From National Research Council Canada

DOIResolve DOI: https://doi.org/10.1016/j.compstruct.2015.12.025
AuthorSearch for: ; Search for: ; Search for: 1; Search for: 1
  1. National Research Council of Canada. Aerospace
FormatText, Article
SubjectDrops; Laminated composites; Stiffness; Strain; Compression buckling; Compression loading; Fiber placement; Gaps/overlaps; Geometric curvature; Out-of-plane deflection; Structural performance; Variable stiffness; Buckling
Publication date
Peer reviewedYes
NPARC number21277438
Export citationExport as RIS
Report a correctionReport a correction (opens in a new tab)
Record identifierd9180ed2-4910-4ffa-9087-234793ea5338
Record created2016-03-09
Record modified2020-04-22
Date modified: